宇航材料工艺
宇航材料工藝
우항재료공예
AEROSPACE MATERIALS & TECHNOLOGY
2009年
6期
19-22
,共4页
叶丽%陈于蓝%韩伟健%冀志宏%赵彤
葉麗%陳于藍%韓偉健%冀誌宏%趙彤
협려%진우람%한위건%기지굉%조동
SiO_2%酚醛%复合气凝胶
SiO_2%酚醛%複閤氣凝膠
SiO_2%분철%복합기응효
SiO_2%Resorcinol-formaldehyde%Composite aerogels
以间苯二酚(R)和甲醛(F)为碳源,以3-胺丙基三乙氧基硅烷(APTES)为硅源,一步溶胶一凝胶法简单快捷地合成了SiO_2-RF复合气凝胶,高温碳化后得到SiO_2-C复合气凝胶,并用扫描电镜、比表面分析仪对所得样品的结构进行了研究,并讨论了不同投料比对气凝胶结构的影响.结果表明碳化前,投料比APTES/R=1时,所得气凝胶具有最大的比表面积(S_(BET)=606.1 m~2/g),碳化后,由于体积收缩和酚醛热解产生新孔隙双重因素的影响,投料比AFTES/R=1/2时样品的比表面积达到最大(S_(BET)=704.2 m~2/g).
以間苯二酚(R)和甲醛(F)為碳源,以3-胺丙基三乙氧基硅烷(APTES)為硅源,一步溶膠一凝膠法簡單快捷地閤成瞭SiO_2-RF複閤氣凝膠,高溫碳化後得到SiO_2-C複閤氣凝膠,併用掃描電鏡、比錶麵分析儀對所得樣品的結構進行瞭研究,併討論瞭不同投料比對氣凝膠結構的影響.結果錶明碳化前,投料比APTES/R=1時,所得氣凝膠具有最大的比錶麵積(S_(BET)=606.1 m~2/g),碳化後,由于體積收縮和酚醛熱解產生新孔隙雙重因素的影響,投料比AFTES/R=1/2時樣品的比錶麵積達到最大(S_(BET)=704.2 m~2/g).
이간분이분(R)화갑철(F)위탄원,이3-알병기삼을양기규완(APTES)위규원,일보용효일응효법간단쾌첩지합성료SiO_2-RF복합기응효,고온탄화후득도SiO_2-C복합기응효,병용소묘전경、비표면분석의대소득양품적결구진행료연구,병토론료불동투료비대기응효결구적영향.결과표명탄화전,투료비APTES/R=1시,소득기응효구유최대적비표면적(S_(BET)=606.1 m~2/g),탄화후,유우체적수축화분철열해산생신공극쌍중인소적영향,투료비AFTES/R=1/2시양품적비표면적체도최대(S_(BET)=704.2 m~2/g).
SiO_2 - RF composite aerogels were prepared by one-step sol-gel method by using resorcinol ( R), formaldehyde (F) and 3-aminopropyltriethoxylsilane (APTES) as starting materials. After carbonization, SiO_2 - C composite aerogels were obtained. The structure of the aerogels was characterized by scanning electron microscopy and nitrogen adsorption/desorption analysis. The structure of SiO_2 - RF snd SiO_2 - C composite aerogels are strongly de-pendent on the APTES/R molar ratio. When APTES/R = 1, SiO_2 - RF composite aerogel has the highest specific sur-face area S_(BET)(606. 1 m~2/g). However,the highest specific surface area S_(BET)(704.2 m~2/g) is obtained when APTES/ R = 1/2 after carbonization for two reason:volume shrinkage and new pore come into being.